The impact of weak shock waves on the flow in the boundary layer of a flat plate with a variable sweep angle of the leading edge

Research output: Contribution to journal › Article › peer-review

Original language	English
Pages (from-to)	803-809
Number of pages	7
Journal	Thermophysics and Aeromechanics
Volume	26
Issue number	6
DOIs	https://doi.org/10.1134/S0869864319060027
Publication status	Published - 1 Nov 2019

leading blunt edge, longitudinal vortex, N-wave, supersonic boundary layer, swept plate, COUPLE, MACH WAVE, LAMINAR-TURBULENT TRANSITION

ID: 23666009